NASA NTRS · 19910011926
Solid rocket booster internal flow analysis by highly accurate adaptive computational methods
Abstract
The primary objective of this project was to develop an adaptive finite element flow solver for simulating internal flows in the solid rocket booster. Described here is a unique flow simulator code for analyzing highly complex flow phenomena in the solid rocket booster. New methodologies and features incorporated into this analysis tool are described.
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Huang, C. Y., Tworzydlo, W., Oden, J. T., Bass, J. M., Cullen, C., Vadaketh, S.. 1991-03-15. Solid rocket booster internal flow analysis by highly accurate adaptive computational methods. https://ntrs.nasa.gov/citations/19910011926
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